GB534529A - Improvements relating to variable-pitch airscrews - Google Patents
Improvements relating to variable-pitch airscrewsInfo
- Publication number
- GB534529A GB534529A GB2172339A GB2172339A GB534529A GB 534529 A GB534529 A GB 534529A GB 2172339 A GB2172339 A GB 2172339A GB 2172339 A GB2172339 A GB 2172339A GB 534529 A GB534529 A GB 534529A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pitch
- piston
- spring
- blades
- oil
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/32—Blade pitch-changing mechanisms mechanical
- B64C11/36—Blade pitch-changing mechanisms mechanical non-automatic
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Transmission Devices (AREA)
Abstract
534,529. Variable pitch propellers. DE HAVILLAND AIRCRAFT CO., Ltd., and THOMAS, F. M. July 26, 1939, No. 21723. [Class 114] Energy is accumulated during pitch-change operations outside the normal range of pitch variation, and is used to effect such abnormal pitch variations, e.g. feathering and unfeathering. The pitch may be changed by a piston 7 carrying racks engaging pinions on the blades. This piston is actuated by oil under pressure supplied through an annular space 22 in the screw shaft, between a fixed seating 21 and a seating on a piston 16 which is moved against a spring 17 by oil under pressure supplied through a conduit 18. When the pressure in the conduit 18 is cut off, the spring 17 returns the piston, and the seats 20, 21 are pressed into contact, the entrapped oil holding the piston in position against a spring 9, and also when the blades are moved into feathering position, against a spring 10. On reopening the lock 20, 21, the release of oil pressure allows the springs to return the blades to normal pitch. The oil pressure is used indirectly to press the rack and pinion into contact. Specification 509,298 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2172339A GB534529A (en) | 1939-07-26 | 1939-07-26 | Improvements relating to variable-pitch airscrews |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2172339A GB534529A (en) | 1939-07-26 | 1939-07-26 | Improvements relating to variable-pitch airscrews |
Publications (1)
Publication Number | Publication Date |
---|---|
GB534529A true GB534529A (en) | 1941-03-10 |
Family
ID=10167755
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2172339A Expired GB534529A (en) | 1939-07-26 | 1939-07-26 | Improvements relating to variable-pitch airscrews |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB534529A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3393748A (en) * | 1966-07-22 | 1968-07-23 | United Aircraft Corp | Propeller with spring actuated variable pitch |
US4037986A (en) * | 1975-09-04 | 1977-07-26 | Dowty Rotol Limited | Bladed rotors having control means for effecting blade pitch adjustment |
US6478542B1 (en) * | 2001-04-19 | 2002-11-12 | Morris C. Elliott | Variable pitch propeller having centrifugal lock |
-
1939
- 1939-07-26 GB GB2172339A patent/GB534529A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3393748A (en) * | 1966-07-22 | 1968-07-23 | United Aircraft Corp | Propeller with spring actuated variable pitch |
DE1531551B1 (en) * | 1966-07-22 | 1969-11-06 | United Aircraft Corp | Blade angle adjustment device for propellers |
US4037986A (en) * | 1975-09-04 | 1977-07-26 | Dowty Rotol Limited | Bladed rotors having control means for effecting blade pitch adjustment |
US6478542B1 (en) * | 2001-04-19 | 2002-11-12 | Morris C. Elliott | Variable pitch propeller having centrifugal lock |
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